function T = DisplayManeuverInformation(DelVs,maneuverstart_UTC,maneuverfinish_UTC,maneuvertype,ManeuverMass,ManeuverDuration,UTCStart)

N = length(DelVs);

ManeuverDuration_sec = zeros(N,1);
ManeuverDuration_hour = zeros(N,1);
for ii = 1:N
    ManeuverDuration_sec(ii) =etime(maneuverfinish_UTC(ii,:),maneuverstart_UTC(ii,:));
    ManeuverDuration_hour(ii) = ManeuverDuration_sec(ii)/3600; 
    
end

driftTime(1) = etime(maneuverfinish_UTC(1,:),UTCStart);

for ii = 2:N
   driftTime(ii) = etime(maneuverfinish_UTC(ii,:),maneuverfinish_UTC(ii-1,:));
end

Maneuvers = linspace(1,N,N)';
T = table(Maneuvers,DelVs,maneuvertype,ManeuverMass,ManeuverDuration,driftTime');

end